A missile or rocket comprising two parts which are separable along trajectory

A flying machine, particularly a missile, comprising two parts (20, 30), a front part (20) and a rear part (30) respectively, intended to be separated along trajectory, characterized in that it further comprises an asymmetric canopy (50) linked to the rear part (30) and making it possible to ensure...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PHILIPPE MOURRY, MARC PINOL
Format:	Patent
Sprache:	eng
Schlagworte:	AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
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